TM 55-1560-307-13&P Table 2-1.  ERFS Components (Cont) NOMENCLATURE PART NUMBER NSN QTY Hose Assy AE706285-6 4720-01-214-1001 1 Hose Assy MS28741-24D-0160 . . . 1 Hose Assy 390A-16D-0720 . . . 4 Identical Tee 180-950248-16D-0360 Hose Assy . . . 1 Panel Assy (FMCP) 85SDSCC-D-0007-100 . . . 1 Plywood Deck 85SDSCC-D-0007-187 . . . 8 Shoring Pump Assy 85SDSCC-D-0007-101 . . . 4 Quick Disconnect 114PS491-2 4730-01-140-6760 2 Reducer, Tube MS24399D28 4730-01-262-8293 1 Strap, Webbing SP4212-1 1670-00-725-1437 38 Strap, Webbing B-D-10000 R/0-234-HH-24 5340-01-233-3063 8 Wrench 1232 5120-00-203-4812 1 Wrench 1248 5120-00-203-4804 1 Wrench 1244 5120-00-203-4806 1 Wrench 1240 5120-00-203-4808 1 Wrench 1252 5120-00-203-4802 1 Section II.  INSPECTING THE EQUIPMENT 2-4.  INSPECTION.    Inspect  the  ERFS  components  as follows: CAUTION A   daily   visual   inspection   shall   be made   of   the   subject   installation   to ensure that no progressive structural deterioration  is  occurring,  that  there is  no  loss  of  security,  and  that  no damage  to  the  host  helicopter,  tank fittings,   tiedown   straps,   etc.,   exist. Any    occurrence    of    the    preceding shall   be   corrected   prior   to   further flight operations. a.  Initial Installation.  The ERFS will be inspected after initial installation in the aircraft. b.    When  system  components  have  been  out  of service for a period of 7 days or more. c.  When maintenance has been preformed on any part    or    component    of    the    system    to    correct    a malfunction. d.  When the ERFS tank system has been purged in  accordance  with  instructions  provided  in  Chapter  3, Section V, para 3-25 of this manual. e.  Before each flight, check system in accordance with the PMCS, Table 2-6. f.    Immediately  after  fueling  system,  inspect  for leaks. 2-2